P-401.pdf
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- Solicitation number
- N6134019R0007
About this file
This document provides an amendment to a Navy solicitation seeking an Advanced Helicopter Training System and TH-XX aircraft. The amendment disseminates responses to potential offeror questions and incorporates updates to the solicitation, including a revised Performance Work Statement and Access Agreement. The offer due date remains unchanged. The Naval Air Systems Command seeks these products and services to support helicopter pilot training. Interested parties should review the conformed solicitation copy for updated requirements and instructions.
P-401
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Text version
rho
Adjustment DA Max Gross Wt (HOGE)
NONE 7800 FT 34,800 lbs
10% RULE 8800 FT 34,000 lbs
DA COMPUTER 8400 FT 34,500 lbs
40% RULE 8400 FT 34,500 lbs m
T omega
FF SCVqSCAF Vq
LL SCVqSCL Vq
DD SCVqSCD Vq
SCVL V
lSCVL V bcRAS bA b c R
R bc
R bcR
A Ab
RR
bbA bA A
RA
T
A A
RA
Tc bb
T
AbA
Therefore, the student is expected to become familiar with all NATOPS performance charts prior to class.
VA2
T=Power fDisk induced
A
A2 ThrustxThrust=Power disk induced
A
A2 Thrust=v disk i A
ThrustxThrust=Power disk induced
A everybody else skip this part cdrRCP D
R
O ofile R
R
O drRcCP R
O Dofile
R
O c
RcCP Dofile c b=
PTotal = P Induced + P Profile ihffinduced VVVV V ih A
ThrustV dA
VA2
T=V fDisk induced
A fDisk induced VA
TPower
DAD
Rx
VelocityTipBlade AircraftofVelocity=ratio)(advance xx (a b= b tipDdProfile )4.65+(1VAC8 1=Power
VRS
Region
Thrust=v i A
PvTP i
(b) Low Inertia .
thrustrotortotal componentverticalAOB v
AOB
componentverticalthrustrotortotal v nWLor W Ln nW
W L gg g
Vr nga m ngm m gma gmW ngmT m T m W m T m Wa
TWmaF
Z
Z
Z
ZZ
tav Z ta tad v ta mk ftlbMass ftlbsStiffness
2 2
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